View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 40025U 14033R 25166.70292309 .00006424 00000-0 39279-3 0 9993
2 40025 98.0828 149.6352 0011414 42.1742 318.0362 15.10579810597561
| Epoch (UTC): | 15 June 2025 16:52:12 |
| Eccentricity: | 0.0011414 |
| inclination: | 98.0828° |
| perigee height: | 526 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 149.6352° |
| argument of perigee: | 42.1742° |
| revolutions per day: | 15.10579810 |
| mean anomaly at epoch: | 318.0362° |
| orbit number at epoch: | 59756 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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